EP3262268B1

EP3262268B1 - Seal assemblies for earth boring drill bits, drill bits so equipped, and related methods

Info

Publication number: EP3262268B1
Application number: EP16756454.1A
Authority: EP
Inventors: Jon D. SCHRODER
Original assignee: Baker Hughes Inc; Baker Hughes a GE Co LLC
Current assignee: Baker Hughes Holdings LLC
Priority date: 2015-02-27
Filing date: 2016-02-26
Publication date: 2020-01-15
Anticipated expiration: 2036-02-26
Also published as: CA2977797C; SG11201706979RA; US20160251903A1; EP3262268A4; US10458187B2; CN107407130A; WO2016138393A1; EP3262268A1; MX2017010963A; CN107407130B; CA2977797A1

Description

TECHNICAL FIELD

Embodiments of the present disclosure relate to earth-boring tools for drilling boreholes, and to seal assemblies utilized in such tools.

BACKGROUND

Earth-boring tools are used to form boreholes (e.g., wellbores) in subterranean formations. Some earth-boring tools, such as roller cone drill bits and hybrid drill bits, include a rotational bearing between a non-rotating member and a rotating member such as a roller cone including cutting elements. A bearing seal may protect the bearing by inhibiting the ingress of drilling fluid and formation cuttings to the bearing, and by at least partially preventing discharge of lubricant (e.g., grease) used to lubricate both the bearing and the seal. One type of seal used in such tools employs primary metal-to-metal face seals that are energized by, e.g., an elastomeric ring. Such a seal may be referred to as a rigid face seal or a metal face seal. Such seals may include at least one rigid ring having a seal face thereon, and an energizing element, which urges the seal face of the rigid ring into sealing engagement with a second sealing face. One or both of the sealing faces may be coated with a wear-resistant coating, such as diamond-like carbon (DLC). Embodiments of such bearing seals are disclosed in U.S. Patent No. 7,413,037 to Lin et al., issued Aug. 19, 2008 , and assigned to the assignee of the present disclosure (the '037 Patent).
As disclosed in the '037 Patent, the rigid ring may be confined in a groove near the base of the shaft on which the roller cone is rotatably affixed. The second sealing face may be disposed on a sealing element (e.g., a steel ring) pressed into a cavity of the roller cone, and the energizing element may be located adjacent the base of the shaft and circumferentially inward from the rigid ring. Such an arrangement may require a certain minimum axial length of the bearing and seal assembly. Furthermore, relative rotational movement between the energizing element and one or both of the rigid ring and the shaft may occur in the event that the rigid ring sticks to the sealing element in the roller cone, resulting in poor sealing and rapid degradation of the energizing element. Finally, if an inward force is applied to the roller cone (i.e., a force urging the cone radially inward toward a rotational axis of a body of the bit) the biasing force provided by the energizing element may be reduced, compromising the seal and allowing lubricant to leak from the seal and/or allowing drilling fluid and formation cuttings to contaminate the bearing.
US 3193028 , over which the independent claim is characterized, discloses a rotary drill bit.

DISCLOSURE

According to one aspect the present invention provides an earth-boring tool as claimed in claim 1.
The earth-boring tool may comprise a drill bit which includes the bit body, and the rotating member may be a cone. The second sealing surface may be affixed to the bit body and may face generally radially outward from an axis of rotation of the bit body.
According to another aspect the present invention provides a method of assembling a drill bit as claimed in claim 16.

BRIEF DESCRIPTION OF DRAWINGS

While the specification concludes with claims particularly pointing out and distinctly claiming what are regarded as embodiments of the disclosure, various features and advantages of disclosed embodiments may be more readily ascertained from the following description when read with reference to the accompanying drawings, in which:

FIG. 1 is a cross-sectional view of an earth-boring tool according to an embodiment of the disclosure;
FIG. 2 is an enlarged cross-sectional view of a seal assembly of the earth-boring tool of FIG. 1; and
FIG. 3 is an enlarged cross-sectional view of an earth-boring tool with a seal assembly according to another embodiment of the disclosure.

MODE(S) FOR CARRYING OUT THE INVENTION

The illustrations presented herein are not actual views of any particular material, earth-boring tool, or component thereof, but are merely idealized representations employed to describe embodiments of the present disclosure. Additionally, elements common between figures may retain the same numerical designation.
Embodiments of the disclosure include bearing seals configured to inhibit leakage of lubricant from and ingress of drilling fluid and formation cuttings to rotational bearings in earth-boring tools. In particular, embodiments of bearing seals of the disclosure minimize (e.g., reduce) axial space requirements of the seal, simplify manufacturing and assembly, and improve reliability of bearing seals as compared to conventional bearing seal designs, as discussed below.
FIG. 1 shows a cross-sectional view of an embodiment of an earth-boring tool 100 according to the disclosure. The earth-boring tool 100 shown is a hybrid roller-cone/fixed cutter drill bit having a bit body 102, and includes a threaded pin connection 104 configured for connection to a box section at a distal end of a drilling assembly, e.g., a drill string (not shown). In the embodiment of FIG. 1, the bit body 102 is shown with a separate shank 105 carrying the threaded pin connection and affixed (e.g., welded) to the bit body 102. In other embodiments, the shank 105 and bit body 102 may be integral (i.e., a single unitary component). The bit body 102 includes a plurality of legs 106, each carrying a shaft 108 protruding radially inward from the corresponding leg 106 (i.e., depending generally toward a rotational axis AB of the bit body 102) at an acute included angle relative to rotational axis AB. Each shaft 108 carries a respective cone 110, the shaft 108 being inserted within a cavity 112 of each respective cone 110. Each cone 110 includes a plurality of cutting elements, which are commonly characterized as " inserts" 111 comprising a material such as tungsten carbide, having a portion or portions coated with, for example, a superabrasive material such as polycrystalline diamond or cubic boron nitride. Other materials having sufficient hardness and abrasion-resistance to remove material from a subterranean formation under applied weight on bit may be employed. In some embodiments, inserts 111 may be integral with a cone 110. A bearing assembly 114 may be disposed between a surface of the cone 110 within the cavity 112 and the shaft 108.
As a non-limiting example, and as shown in the embodiment of FIG. 1, the bearing assembly 114 may be a tapered roller bearing including an inner bearing race 116, a plurality of rollers 118, and an outer bearing race 120. The inner bearing race 116 may be configured for a non-interference fit (e.g., a slip fit) over the shaft 108, and the cone 110 and bearing assembly 114 may be retained on the shaft 108 by a tension rod 122 retained within a bore 124 of the shaft 108 by, e.g., a threaded nut 126 engaged with the tension rod 122. In the embodiment shown in FIG. 1, a secondary tapered roller bearing assembly 115 is disposed between the cone 110 and the shaft 108. In other embodiments, the bearing configuration may include one or more plain bearings (e.g., journal bearings) or other bearing configurations. For example, in some embodiments, the inner bearing race 116 may include a bearing journal, and the outer bearing race 120 may include a bearing surface configured to rotate against the journal of the inner bearing race 116.
A lubricant (e.g., grease) may be supplied to the bearing assembly 114 from a pressure-compensating lubrication system 128 through a lubricant passageway 130. A seal assembly 132 is disposed between a surface of the inner bearing race 116 and a surface of the cone 110 within the cavity 112, and prevents the flow of lubricant away from the bearing assembly 114. The seal assembly 132 also prevents ingress of drilling fluid and formation cuttings into the cavity 112 of the cone 110 to extend the life of the bearing assembly 114.
In use, the earth-boring tool 100 is advanced in a borehole by rotating the drill string (not shown), by rotating the earth-boring tool 100 with, e.g., a mud motor of a bottom-hole assembly (BHA), or both. As the earth-boring tool 100 rotates and weight or other axial force is applied to the drill string, the cones 110 rotate on corresponding shafts 108 (i.e., rotate about a secondary rotational axis AC) and the cutting elements 111 engage and degrade the formation with a crushing and grinding action.
Referring now to FIG. 2, an enlarged cross-sectional view of a seal assembly 132 of the disclosure is shown. In embodiments of the disclosure, one or more components of the seal assembly 132 as described below may be at least partially disposed within a bearing retainer 134. The bearing retainer 134 may be threaded, pressed, brazed, or otherwise affixed within the cavity 112 of the cone 110. The bearing retainer 134 may abut at least a portion of the outer bearing race 120 to retain the outer bearing race 120 within the cavity 112 of the cone 110. In some embodiments, the bearing retainer 134 may include a flange (i.e., an annular protrusion) 136 configured to retain one or more components of the seal assembly 132 at least partially within the bearing retainer 134. The bearing retainer 134 and one or more components of the seal assembly 132 may be rotationally coupled with (i.e., rotate together with) the cone 110 about the secondary rotational axis AC.
For example, a sealing element 138 may be rotationally coupled with the cone 110. In other words, the sealing element 138 may rotate with the cone 110 as the cone 110 rotates on the shaft 108 about the secondary rotational axis AC. The sealing element 138 may comprise a metal alloy, such as steel, and may undergo thermal processing (e.g., heat treatment) to provide desired material characteristics such as a particular hardness value. In other embodiments, the sealing element 138 may comprise other metals, alloys, or non-metal materials (e.g., polymers). The sealing element 138 may have a substantially annular shape with a generally trapezoidal cross-section in a plane parallel with the rotational axis of the cone 110 and sealing element 138 (e.g., the cross-sectional plane of FIG. 2). The sealing element 138 may also be characterized as a "sealing ring." The sealing element 138 includes a first sealing surface 140. The first sealing surface 140 may be processed (e.g., ground, lapped, polished, etc.) to impart to the first sealing surface 140 a desired profile and surface finish.
The first sealing surface 140 is urged into sealing engagement with a second sealing surface 142. In other words, contact between the first sealing surface 140 and the second sealing surface 142 may impede intrusion of drilling fluid and/or formation cuttings between the first sealing surface 140 and the second sealing surface 142 and may prevent leakage of lubricant from the bearing assembly 114 (FIG. 1). The second sealing surface 142 may be disposed on a portion of the bit body 102 (FIG. 1), or may be disposed on a component affixed to the bit body 102. The second sealing surface 142 may remain stationary relative to the cone 110. In other words, the second sealing surface 142 may not rotate with the cone 110 as the cone 110 rotates about the secondary rotational axis AC. For example, in the embodiment of FIG. 2, the second sealing surface 142 may be disposed on a portion of the inner bearing race 116, and the inner bearing race 116 may be affixed to the shaft 108 of the bit body 102 (FIG. 1). The second sealing surface 142 may face generally radially outward with respect to the rotational axis AB (FIG. 1) of the bit body 102. In other words, the second sealing surface may be positioned inboard from an associated leg 106 (FIG. 1) of the bit body 102 and generally face the associated leg 106. The second sealing surface 142 may be processed (e.g., ground, lapped, polished, etc.) to impart to the second sealing surface 142 the desired profile and surface finish.
In some embodiments, one or both of the first sealing surface 140 and the second sealing surface 142 may comprise a wear-resistant coating. For example, one or both of the first sealing surface 140 and the second sealing surface 142 may comprise a coating of diamond-like carbon (DLC) material. In one exemplary embodiment, the second sealing surface 142 of the inner bearing race 116 may comprise a DLC coating, and the first sealing surface 140 may not include a surface coating. In other embodiments, one or both of the first sealing surface 140 and the second sealing surface 142 may include other wear resistant materials such as, for example, polycrystalline diamond material.
The seal assembly 132 includes an energizing element 144. The energizing element 144 may be said to "energize" the seal in the sense that the energizing element 144 provides a biasing force that urges the first sealing surface 140 of the sealing element 138 into sealing engagement with the second sealing surface 142 of the inner bearing race 116. For example, the energizing element 144 may comprise an elastomeric material compressively strained between the sealing element 138 and the bearing retainer 134. As a non-limiting example, the energizing element 144 may be an O-ring comprising a nitrile material. The energizing element 144 may be substantially annular and have a circular, oval, elliptical, or other undeformed cross-sectional shape. Compressively straining the energizing element 144 between the sealing element 138 and the bearing retainer 134 may create a biasing force urging the sealing element 138 into sealing engagement with the second sealing surface 142 of the inner bearing race 116 as the energizing element 144 attempts to return to an undeformed configuration. For example, the energizing element 144 may have a substantially circular undeformed cross-sectional shape, and compressive strain applied to the energizing element 144 as the energizing element 144 is compressed between the sealing element 138 and the bearing retainer 134 may impart to the energizing element 144 a substantially ovoid cross-sectional shape, as shown in FIG. 2.
The energizing element 144 may be located radially outward from the sealing element 138. For example, as shown in FIG. 2, the energizing element 144 may substantially circumferentially surround a generally frustoconical surface 139 of the sealing element 138 that faces generally radially outward from the sealing element 138 with respect to the secondary rotational axis AC. Such an arrangement may provide advantages over some conventional seal arrangements. For example, in some conventional designs, an energizing element may be located radially inward from a sealing element, such that the contact area between the sealing face of the sealing element and a sealing surface on the cone occurs at a greater radial distance from the axis of rotation of the cone than does contact between the sealing element and the elastomeric energizing element. Accordingly, in such a conventional design, the contact area between the sealing element and the energizing element may be insufficient to prevent the sealing element from "sticking" to the sealing element in the cone (i.e., rotating with the cone) under certain conditions. If the sealing element begins to rotate with the cone, the seal between the sealing element and the sealing element in the cone may be compromised. Furthermore, relative rotational movement between the energizing element and the sealing element may quickly degrade the energizing element. In contrast, in embodiments of the disclosure, the energizing element 144 may be positioned radially outward from the sealing element 138, increasing the contact area between the energizing element 144 and the sealing element 138, and preventing the sealing element 138 from "sticking" to the second sealing surface 142 of the inner bearing race 116.
In some embodiments, the seal assembly 132 may include a secondary seal element 146 disposed at least partially in the flange 136 of the bearing retainer 134. The secondary seal element 146 may comprise an elastomer or other material, and may have a shape configured to provide a seal between the flange 136 of the bearing retainer 134 and the sealing element 138 to prevent leakage of lubricant and ingress of drilling fluid and formation cuttings to the bearing assembly 114 (FIG. 1). A portion of the sealing element 138 opposite the first sealing surface 140 may abut the secondary seal element 146. The secondary seal element 146 may comprise, e.g., an elastomeric material.
A static seal 148 may be disposed between a surface of the shaft 108 and the inner bearing race 116. In the embodiment shown in FIG. 2, the static seal 148 may be an O-ring disposed in a groove 150 in the surface of the shaft 108. As the inner bearing race 116 may have a non-interference fit (e.g., a slip fit) over the shaft 108 to ease assembly, the static seal 148 may prevent intrusion of drilling fluid and formation cuttings between the inner bearing race 116 and the shaft 108 and eventual contamination of the bearing assembly 114. Similarly, the static seal 148 may prevent leakage of the lubricant from the bearing assembly 114.
Assembly of the seal assembly 132 may proceed as follows. The bearings 114, 115 (FIG. 1), and the tension rod 122 (FIG. 1) may be inserted within the cavity 112 of the cone 110. The sealing element 138, the energizing element 144, and the secondary seal element 146 may be placed within the flange 136 of the bearing retainer 134, and the bearing retainer may be affixed within (e.g., threadedly engaged with, pressed into, brazed within, etc.) the cavity 112 of the cone 110, so that the bearing retainer 134 abuts the outer bearing race 120 and the sealing element 138 is brought into sealing engagement with the inner bearing race 116, as described above. The tension rod 122 is then inserted within the bore 124 of the shaft 108, the inner race 116 is guided over the shaft 108, and the nut 126 (FIG. 1) may be tightened over the tension rod 122 to retain the cone 110 over the shaft 108 and provide appropriate preload to the bearings 114 and 115.
In some embodiments, a seal assembly according to the disclosure may include a sealing element and an energizing element formed as a unitary component. For example, in some embodiments, the seal assembly may include a unitary component including both an energizing element and a sealing element. The unitary component may comprise, e.g., a metal alloy. Such unitary energizing elements and sealing elements may be similar to the metallic seals disclosed in U.S. Patent App. Pub. No. 2014/0326514 A1 to Lin et al., published Nov. 6, 2014 and assigned to the assignee of the present disclosure.
Furthermore, in some embodiments, the unitary sealing element and energizing element may be formed integrally with a bearing retainer. For example, FIG. 3 shows another embodiment of a seal assembly 150 according to the disclosure. The seal assembly 150 may include an elastically deformable energizing element 154 depending radially inward from a bearing retainer 152 with respect to the secondary rotational axis AC. The energizing element 154 may be formed integrally with the bearing retainer 152. A sealing element 156 may be formed integrally with the energizing element 154 and may depend radially inward from the energizing element 154 with respect to the secondary rotational axis AC. The bearing retainer 152, the energizing element 154, and the sealing element 156 may comprise a metal alloy such as, e.g., steel.
The sealing element 156 may include a first sealing surface 158 in sealing engagement with a second sealing surface 160 disposed on the inner bearing race 116. As described above in connection with FIG. 2, one or both of the first sealing surface 158 and the second sealing surface 160 may include a wear-resistant coating, e.g., DLC, or other wear-resistant materials.
The energizing element 154 may be configured to provide a biasing force that urges the first sealing surface 158 of the sealing element 156 into sealing engagement with the second sealing surface 160 of the inner race 116. For example, the energizing element 154 may be configured to elastically deform when the bearing retainer 152 is installed within the cone 110 and the first sealing surface 158 contacts the second sealing surface 160. Mechanical contact between the first sealing surface 158 and the second sealing surface 160 may prevent the energizing element 154 from returning to an undeformed configuration, thus producing a biasing force urging the first sealing surface 158 into contact with the second sealing surface 160.
In some embodiments, the energizing element 154 and the sealing element 156 may be formed integrally, and may be affixed to a bearing retainer 152 formed separately from the integral energizing element 154 and sealing element 156. For example, the energizing element 154 and the sealing element 156 may be integrally formed and pressed or brazed within a seat (e.g., recess) formed in a separate bearing retainer. The integral energizing element 154 and sealing element 156 may comprise a metal alloy the same or different from a metal alloy of which the bearing retainer 152 is comprised.
Compared to some conventional seal designs, embodiments of bearing seals according to the disclosure may occupy less axial space in the cone, require fewer components and assembly steps, and exhibit improved reliability and sealing performance. For example, seal assemblies of the disclosure do not require a separate sealing element pressed into the cone, and accordingly occupy less axial space by comparison, enabling a reduction in the cutting diameter of the earth-boring tool 100. Furthermore, elimination of the separate sealing element pressed in the cone simplifies manufacturing and assembly of the earth-boring tool 100.
Moreover, locating the sealing element 138 (FIG. 2) or 156 (FIG. 3) and the energizing element 144 (FIG. 2) or 154 (FIG. 3) at least partially within the cone 110 and configuring the sealing element 138, 156 and energizing element 144, 154 to rotate with the cone 110 about the secondary rotational axis AC as described above may improve reliability of the seal compared to conventional seal designs in which the seal assembly is located on the shaft of the bit body and the sealing element does not rotate with the cone. For example, in such conventional designs, when a cone is subject to a force directed radially inward with respect to the bit body (in other words, a force tending to pull the cone away from an associated leg of the bit body and inward toward a rotational axis of the bit body), compressive strain on an energizing element may be reduced and a biasing force generated by the energizing element lessened accordingly. Under these conditions, the biasing force may be insufficient to maintain sealing engagement between the sealing element and a sealing surface of the cone, allowing leakage of lubricant and ingress of drilling fluid and formation cuttings to the bearing. In contrast, in embodiments of the disclosure, when the cone 110 (FIG. 2) is subject to a force directed radially inward toward the rotational axis AB (FIG. 1) of the bit body 102 (FIG. 1), contact between the sealing element 138 (FIG. 2) and the inner bearing race 116 (FIG. 2) urges the generally frustoconical surface 139 of the sealing element 138 against the energizing element 144 (FIG. 2), increasing the biasing force urging the sealing element 138 against the second sealing surface 142. Thus, embodiments of the disclosure maintain integrity of the seal even when such inward forces are applied to the cone 110.
Although the foregoing description and accompanying drawings contain many specifics, these are not to be construed as limiting the scope of the disclosure, but merely as describing certain embodiments. Similarly, other embodiments may be devised, which do not depart from the scope of the disclosure. For example, features described herein with reference to one embodiment also may be provided in others of the embodiments described herein. The scope of the invention is, therefore, indicated and limited only by the appended claims.

Claims

An earth-boring tool, comprising:
a body (102);

a rotating member (110) disposed over a protrusion (108) from the body (102) and configured to rotate relative to the body (102);

a bearing assembly (114) disposed within a cavity (112) of the rotating member (110), the bearing assembly (114) comprising an inner race (116) coupled with the protrusion (108) and an outer race (120) coupled with the rotating member (110); and

a bearing retainer (134) affixed within the cavity (112) of the rotating member (110) and retaining the bearing assembly (134) within the cavity (112) of the rotating member (110); characterized in that the earth-boring tool further comprises:

a seal assembly (132) comprising:
a sealing element (138) rotationally coupled with the bearing retainer (134), the sealing element (138) comprising a first sealing surface (140);

a second sealing surface (142) disposed on the inner race (116); and

an energizing element (144) urging the first sealing surface (140) into sealing engagement with the second sealing surface (142).
The earth-boring tool of claim 1, wherein the bearing retainer (134) comprises a flange (136), and wherein the sealing element (138) is retained between the flange (136) of the bearing retainer (134) and the second sealing surface (142) when the bearing retainer (134) is installed in the cavity (112) of the rotating member (110).
The earth-boring tool of claim 2, wherein the energizing element (144) is disposed radially outward from a portion of the sealing element (138) and radially inward from a portion of the bearing retainer (134) with respect to a rotational axis about which the rotating member (110) rotates with respect to the body protrusion (108).
The earth-boring tool of claim 3, wherein the energizing element (144) is compressively strained between a portion of the sealing element (138) and a portion of the bearing retainer (134) when the bearing retainer (134) is installed in the cavity (112) of the rotating member (110).
The earth-boring tool of claim 4, wherein the energizing element (144) produces a biasing force urging the first sealing surface (140) of the sealing element (138) into sealing engagement with the second sealing surface (142) of the inner bearing race (116) when the energizing element (144) is compressively strained between the bearing retainer (134) and the sealing element (138).
The earth-boring tool of claim 2, further comprising a secondary seal element (146) disposed between the flange (136) of the bearing retainer (134) and a portion of the sealing element (138) opposite the first sealing surface (140).
The earth-boring tool of claim 6, wherein a portion of the sealing element (138) opposite the first sealing surface abuts the secondary seal element (146).
The earth-boring tool of claim 1, wherein the sealing element (138) and the energizing element (144) are integral.
The earth-boring tool of claim 8, wherein the sealing element (138) and the energizing element (144) are formed from a metal alloy.
The earth-boring tool of claim 9, wherein elastic deformation of the energizing element (144) produces a biasing force maintaining the first sealing surface of the sealing element (138) in sealing engagement with the second sealing surface of the inner race (116) when the bearing retainer (134) is affixed within the cavity of the rotating member.
The earth-boring tool of claim 8, wherein the sealing element (138) and energizing element (144) are integral with the bearing retainer (134).
The earth-boring tool of claim 1, wherein at least one of the first sealing surface (140) and the second sealing surface (142) comprise a wear-resistant coating.
The earth-boring tool of claim 1, further comprising a plurality of rolling bearing elements (118) disposed between the inner race (116) and the outer race (120).
The earth-boring tool of claim 1, wherein the earth-boring tool comprises a drill bit, the protrusion comprises a shaft (108) protruding from a leg (106) of the bit body (102), and the rotating member (110) comprises a roller-cone (110) carrying cutting elements (111).
The earth-boring tool of claim 1, wherein the second sealing surface (140) faces generally radially outward from an axis of rotation of the rotating member (110).
A method of assembling the earth-boring tool of claim 1, the method comprising:
inserting the bearing assembly (114) within the cavity (112) of the rotating member (110);

affixing the bearing retainer (134) comprising the sealing element (138) within the cavity (112) of the rotating member (110);

abutting the sealing element (138) against the inner race (116) of the bearing assembly (114); and

affixing the rotating member (110) over the protrusion (108) from the body (102), wherein the body (110) is one of a roller-cone drill bit and a hybrid drill bit.
The method of claim 16, wherein affixing the bearing retainer (134) comprising the sealing element (138) within the cavity (112) of the rotating member (110) comprises positioning the sealing element (138) between a flange (136) of the bearing retainer (134) and the inner race (116) of the bearing assembly (114).
The method of claim 17, wherein affixing the bearing retainer (134) comprising the sealing element (138) within the cavity (112) of the rotating member (110) comprises compressively straining the energizing element (144) between the bearing retainer (134) and the sealing element (138).
The method of claim 18, wherein affixing the bearing retainer (134) comprising the sealing element (138) within the cavity (112) of the rotating member (110) comprises affixing the bearing retainer (134) comprising an integral energizing element (144) and sealing element (138) within the cavity (112) of the rotating member (110).
The method of claim 19, wherein affixing the bearing retainer (134) comprising the integral energizing element (144) and sealing element (138) within the cavity (112) of the roller cone (110) comprises elastically deforming an integral energizing element (144) comprising a metal alloy.